Investigation of rolling and yawing moments due to ailerons of various chords and spans on two airfoils having Clark Y and U. S. A. 27 wing sections, in 10-ft. wind tunnel of Bureau of Standards on wing models of 60-in. span and 10-in. chord; measurements were made at various angles of pitch but at zero angle of roll and yaw, wing chord being set at angle of plus 4 deg. to fuselage axis.


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    Title :

    Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:
    Heald, R.H. (author) / Strother, D.H. (author) / Monish, B.H. (author)


    Publication date :

    1931


    Size :

    27 pages


    Remarks:

    47 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English